Summary
T21 Definition of TLAR and operations M12In this task the TLAR used for designing the five reference aircraft will be defined by both partners as well as the AB The outcomes will be used to design optimise and assess the aircraft configurations in the WP3 WP4 and WP5 as well as the reference aircraft design and validation in WP3 The initial hypothesis for TLAR will be based on current classleading representative aircraft for each of the five vehicle classes Examples of these include Tecnam P2010 or Pipistrell Panthera GA King Air P180 Avanti Citation or EMB Legacy commuter ATR42ATR72 regional A320A321Neo narrow body A350 wide body Especially for the smaller categories GAcommuter the selection of reference aircraft will be critical and may result in more than 5 reference aircraft in total to cover the broadness of these classes Responsible TUD contribution of TUBST22 Establish matrix of technologies and uncertain parameters M24In this WP the matrix of technologies including airframe propulsion and energy network technologies and propulsive technologies as described in section 131 will be established Besides it will be decided which of these technology parameters will be used as uncertain parametersvariables The decision will be made based on the importance and sensitivity of the technologies on aircraft design and scalability The technologies listed in this table will be implemented at small aircraft level GA then to be developed by upscaling as well as an overview of other radical technologies that may only be applicable in specific classes This provides the basis of T32 T41 and T42 This task will be done collaboratively by both partners and the AB as well as the invitees of the CHYLA first workshop This task involves stage 1 of the scalability assessment ruling out initial options based on existing research and expert judgement Responsible TUBS contribution TUD
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